The Nonlinear Single Controller of DGEN380 Aero Engine Design

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Controlled variable</td><td class="align_center">Proportional gain</td><td class="align_center">Integral gain</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Speed</td><td class="align_center">29.77</td><td class="align_center">5.20</td></tr><tr><td class="align_left">Temperature</td><td class="align_center">33.09</td><td class="align_center">6.55</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>PI controller parameters of the idle power point.</div>

International Journal of Aerospace Engineering

tab2

Table 2

Table 2: The Nonlinear Single Controller of DGEN380 Aero Engine Design 